CN101466592B - 飞机机身结构及其生产方法 - Google Patents

飞机机身结构及其生产方法 Download PDF

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Publication number
CN101466592B
CN101466592B CN2007800211513A CN200780021151A CN101466592B CN 101466592 B CN101466592 B CN 101466592B CN 2007800211513 A CN2007800211513 A CN 2007800211513A CN 200780021151 A CN200780021151 A CN 200780021151A CN 101466592 B CN101466592 B CN 101466592B
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CN
China
Prior art keywords
lower casing
side shell
radius
aircraft fuselage
fuselage structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
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CN2007800211513A
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English (en)
Chinese (zh)
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CN101466592A (zh
Inventor
科德·哈克
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Airbus Operations GmbH
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Airbus Operations GmbH
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Publication date
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Publication of CN101466592A publication Critical patent/CN101466592A/zh
Application granted granted Critical
Publication of CN101466592B publication Critical patent/CN101466592B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Body Structure For Vehicles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
CN2007800211513A 2006-06-06 2007-06-05 飞机机身结构及其生产方法 Expired - Fee Related CN101466592B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102006026170A DE102006026170B4 (de) 2006-06-06 2006-06-06 Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026170.4 2006-06-06
PCT/EP2007/055494 WO2007141251A2 (en) 2006-06-06 2007-06-05 Aircraft fuselage structure and method for its production

Publications (2)

Publication Number Publication Date
CN101466592A CN101466592A (zh) 2009-06-24
CN101466592B true CN101466592B (zh) 2011-07-06

Family

ID=38720942

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2007800211513A Expired - Fee Related CN101466592B (zh) 2006-06-06 2007-06-05 飞机机身结构及其生产方法

Country Status (10)

Country Link
US (1) US8651421B2 (ru)
EP (1) EP2032430B1 (ru)
JP (1) JP2009539672A (ru)
CN (1) CN101466592B (ru)
AT (1) ATE465943T1 (ru)
BR (1) BRPI0712248A2 (ru)
CA (1) CA2654045A1 (ru)
DE (2) DE102006026170B4 (ru)
RU (1) RU2435703C2 (ru)
WO (1) WO2007141251A2 (ru)

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DE102006026170B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
FR2934562B1 (fr) * 2008-07-31 2011-04-22 Airbus France Panneau de protection et module de train d'atterissage le comportant.
CN102126549A (zh) * 2010-01-20 2011-07-20 苏章仁 圆形截面飞行载体壳体顺航向非对称分离仿生结构
AU2011289779B2 (en) * 2010-08-13 2014-01-30 Hexcel Corporation Machinable composite material
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
RU2737210C1 (ru) * 2017-10-11 2020-11-26 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Узел крепления металлической конструкции с конструкцией из полимерных композиционных материалов
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing

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Also Published As

Publication number Publication date
EP2032430B1 (en) 2010-04-28
WO2007141251A3 (en) 2009-01-22
WO2007141251A2 (en) 2007-12-13
DE602007006188D1 (de) 2010-06-10
DE102006026170A1 (de) 2007-12-27
CN101466592A (zh) 2009-06-24
BRPI0712248A2 (pt) 2012-01-17
DE102006026170B4 (de) 2012-06-21
US8651421B2 (en) 2014-02-18
US20090314891A1 (en) 2009-12-24
JP2009539672A (ja) 2009-11-19
RU2008151379A (ru) 2010-07-20
ATE465943T1 (de) 2010-05-15
CA2654045A1 (en) 2007-12-13
RU2435703C2 (ru) 2011-12-10
EP2032430A2 (en) 2009-03-11

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